2015
DOI: 10.1016/j.ymssp.2015.04.020
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Video measurements of instantaneous forces of flapping wing vehicles

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Cited by 11 publications
(6 citation statements)
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“…Additionally, a considerable difficulty is still obtaining realistic experimental data, particularly in free flight and in different flight regimes. Studies have found discrepancies between free-flight and wind tunnel data, 15,16,17 so that realistic insight for free flight ideally should be obtained in free-flight conditions.…”
Section: Introductionmentioning
confidence: 99%
“…Additionally, a considerable difficulty is still obtaining realistic experimental data, particularly in free flight and in different flight regimes. Studies have found discrepancies between free-flight and wind tunnel data, 15,16,17 so that realistic insight for free flight ideally should be obtained in free-flight conditions.…”
Section: Introductionmentioning
confidence: 99%
“…eqs. [8][9][10][11][12][13][14][15][16][17][18][19] were found to converge in the static case, while during flight they vary to a limited extent, typically in conjunction with maneuvers. It can for instance be observed in fig.…”
Section: A Fusion Resultsmentioning
confidence: 94%
“…Additionally, it is still considerably difficult to obtain realistic experimental data, particularly in free flight and in different flight regimes. Studies have found discrepancies between free-flight and wind tunnel data [16,17,18], suggesting that wind tunnel measurements approximate free-flight data only for specific clamping positions and in some flight conditions, so that realistic insight for free flight ideally should be obtained in free-flight conditions.…”
Section: Introductionmentioning
confidence: 99%
“…Recently, the development of external motion tracking systems allowed to estimate the in-flight forces from recorded temporal evolutions of body position and orientation [5], [6], [7]. In general, an agreement has been reported between the in flight estimates and wind tunnel measurements, although differences were found in the direction of the wing stroke [8].…”
Section: Introductionmentioning
confidence: 97%